# Service difficulty reports: N580FE, cancelled Mar 2, 2024

A list on [N580FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N580FE-2024-03-02.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 128 reports

- [SDR FDEA201505081433](https://openairdocs.org/sdr/FDEA201505081433.md): Bottle · discharged · May 8, 2015 · N580FE · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR EMER DOOR OPENING BOTTLE WAS DISCHARGED & SLIDE WAS DISCONNECTED FROM DOOR DURING THE L1 DOOR EMER OPENING. THE SLIDE DID NOT INFLATE.
- [SDR FDEA201502190547](https://openairdocs.org/sdr/FDEA201502190547.md): Bottle · low pressure · Feb 19, 2015 · N580FE · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR ASSIST BOTTLE INDICATES LOW PRESS. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 12-25-04-3-0. OK FOR SERVICE.
- [SDR FDEA201409232715](https://openairdocs.org/sdr/FDEA201409232715.md): Hydraulic Line · leaking · Sep 23, 2014 · N580FE · Doug MD11F · Hydraulic System, Main
  > LEVEL ONE HYD 3 OFF PASSING FL 200 LEVEL TWO HYD 3 FAIL AT FL 370, LOWERED GEAR MANUALLY. FOUND HYD PRESS HOSE THAT CONNECTS FROM THE PYLON TO THE ENG HYD MANIFOLD BLOWN APART AT THE PYLON B NUT. REMOVED THE DAMAGED HOSE. DUE TO NR 3 SYS HYD AT 0 QTY, REQU
- [SDR FDEA201404080697](https://openairdocs.org/sdr/FDEA201404080697.md): Control Unit · failed · Apr 8, 2014 · N580FE · Doug MD11F · Fire Detection
  > ON TAXI OUT RECEIVED LVL 1, FIRE DET 2 FAIL. AFTER STOPPING ACFT, RAN A FIRE TEST & THEN RECEIVED LVL 3, ENG 2 FIRE, ALERT. RAN QRH PROCEDURES, FOR ENG FIRE SEVERE DAMAGE CHECKLIST. FIRED FIRST BOTTLE & ALERT REMAINED ON, AFTER 30 SEC STILL HAD FIRE ALERT O
- [SDR FDEA201305070928](https://openairdocs.org/sdr/FDEA201305070928.md): Skin · misrepaired · May 7, 2013 · N580FE · Doug MD11F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, BS 979, LONGERON 47-48R MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 1 REV 52. EO 1-5100-7- 5001B3, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305060915](https://openairdocs.org/sdr/FDEA201305060915.md): Skin · cracked · May 6, 2013 · N580FE · Doug MD11F · Fuselage Main, Plate/Skin
  > NR 3 AIRCONDITIONING COMPARTMENT AFT UPPER CORNER CUT-OUT SKIN FOUND CRACKED. NR 3 AIRCONDITIONING COMPARTMENT AFT UPPER CORNER CUT-OUT SKIN CARRIED OUT REPAIR IAW SRM 53-20-15, REPAIR 3, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305060919](https://openairdocs.org/sdr/FDEA201305060919.md): Skin · corroded · May 6, 2013 · N580FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING UPPER SURFACE FOUND CORROSION AT XORS 255 DURING SPOILER, UPPER SURFACE INSPECTION. CORROSION REMOVED AND FOUND EXCEED LIMITS IAW SRM 57-20-01, FIG 101, REV 52. DOUBLER REPAIR CARRIED OUT IAW EA 1-5730-167610. REPAIR CLASSIFIED AS MAJOR IAW GMM
- [SDR FDEA201305060916](https://openairdocs.org/sdr/FDEA201305060916.md): Rib · worn · May 6, 2013 · N580FE · Doug MD11F · Leading Edge Devices
  > RT WING NR 4 L/E SLAT INBD SLAT TRACK RIB FWD HOLE FOUND WORN AFTER REMOVAL OF NR 3 SLAT. NR 4 SLAT REWORKED IAW SRM 57-40-02 REPAIR 10, FIGURE 201, REVISION 52. FINAL HOLE DIAMETER 1.125" AND THE CHAFING MARK STILL EXIST, REPAIR ACCOMPLISHED IAW EA 1-5750-
- [SDR FDEA201305040910](https://openairdocs.org/sdr/FDEA201305040910.md): Cap · misrepaired · May 4, 2013 · N580FE · Doug MD11F · Wing Main, Frame Structure
  > LT WING T/E LOWER ACCESS PANEL 541JB CUT-OUT FWD EDGE LOWER CAP MISREPAIRED. REPAIRED IAW EA 1-5710-167609. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305030903](https://openairdocs.org/sdr/FDEA201305030903.md): Rib · cracked · May 3, 2013 · N580FE · Doug MD11F · Leading Edge Devices
  > RIGHT WING NR 5 SLAT FOUND INBD INNER RIB CRACKED. NR 5 SLAT FABRICATED AND INSTALLED IAW EA 1-5750-166127, STEP 2 AND 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305030902](https://openairdocs.org/sdr/FDEA201305030902.md): Support Fitting · damaged · May 3, 2013 · N580FE · Doug MD11F · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR LOWER FRAME SUPPORT FITTING NR 6 HOLE DIAMETER (D) ABOVE THE LIMIT (0.580). R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305030901](https://openairdocs.org/sdr/FDEA201305030901.md): Support Fitting · damaged · May 3, 2013 · N580FE · Doug MD11F · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR LOWER FRAME SUPPORT FITTING NR 1 HOLE DIAMETER ABOVE THE LIMIT (0.580). R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305030900](https://openairdocs.org/sdr/FDEA201305030900.md): Support Fitting · damaged · May 3, 2013 · N580FE · Doug MD11F · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR LOWER FRAME SUPPORT FITTING NR 7 HOLE DIAMETER (A & C) ABOVE THE LIMIT (0.580). R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305030899](https://openairdocs.org/sdr/FDEA201305030899.md): Skin · cracked · May 3, 2013 · N580FE · Doug MD11F · Fuselage Main, Plate/Skin
  > NR 3 AIR CONDITIONING COMPARTMENT AFT UPPER CORNER CUT-OUT SKIN FOUND CRACKED. REPAIRED IAW SRM 53-20-15, REPAIR 3, FIG 201 REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 116.
- [SDR FDEA201305010893](https://openairdocs.org/sdr/FDEA201305010893.md): Beam · corroded · May 1, 2013 · N580FE · Doug MD11F · Fuselage Miscellaneous Structure
  > CENTER WHEEL WELL BS 1461 TO 1490 RT DIAGONAL I-BEAM FOUND CORRODED. R & R WITH NEW FABRICATED I-BEAM IAW SRM 51-31-01, REV 52 AND EA 1-53-167608. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305010892](https://openairdocs.org/sdr/FDEA201305010892.md): Bulkhead · canning · May 1, 2013 · N580FE · Doug MD11F · Fuselage Main, Bulkhead
  > OIL CANNING AT CENTER LANDING GEAR RT VERTICAL WEB BETWEEN BS 1401 TO 1441, Z= -119 TO Z= -83. REPAIRED IAW EO 1-5100-7- 5001B3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305010891](https://openairdocs.org/sdr/FDEA201305010891.md): Bulkhead · canning · May 1, 2013 · N580FE · Doug MD11F · Fuselage Main, Bulkhead
  > OIL CANNING AT CENTER LANDING GEAR LT VERTICAL WEB BETWEEN BS 1401 TO 1441, Z= -119 TO Z= -80. CARRIED OUT INSPECTION IAW EA 1-5310-167604, REPAIRED IAW EO 1-5100-7-5001B3 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304280879](https://openairdocs.org/sdr/FDEA201304280879.md): Skin · cracked · Apr 28, 2013 · N580FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING - L/E LOWER SURFACE NR 12 SLAT TRACK CUT-OUT SKIN FOUND CRACKED AT XOS 777. DURING OTBD SLAT DRIVE CABLES INSPECTION. REPAIRED IAW SRM 57-40-02, FIG 201, REPAIR 7 REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304280878](https://openairdocs.org/sdr/FDEA201304280878.md): Frame · dented · Apr 28, 2013 · N580FE · Doug MD11F · Fuselage Main, Frame
  > BS 1661 LONGERON 12R FRAME FOUND DENTED. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304280877](https://openairdocs.org/sdr/FDEA201304280877.md): Door Frame · cracked · Apr 28, 2013 · N580FE · Doug MD11F · Fuselage Main, Structure
  > L3 DOOR FORWARD FRAME LOWER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304280876](https://openairdocs.org/sdr/FDEA201304280876.md): Door Frame · cracked · Apr 28, 2013 · N580FE · Doug MD11F · Fuselage Main, Structure
  > R3 DOOR AFT FRAME LOWER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304280875](https://openairdocs.org/sdr/FDEA201304280875.md): Door Frame · cracked · Apr 28, 2013 · N580FE · Doug MD11F · Fuselage Main, Structure
  > R3 DOOR FORWARD FRAME WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304260865](https://openairdocs.org/sdr/FDEA201304260865.md): Skin · cracked · Apr 26, 2013 · N580FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING INBD FLAP UPPER SURFACE FOUND CRACKED AT XIFH 177 AND 58" FROM T/E. REPAIRED IAW EA 1-5750-166124. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.
- [SDR FDEA201304260863](https://openairdocs.org/sdr/FDEA201304260863.md): Skin · loose · Apr 26, 2013 · N580FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING INBD FLAP UPPER SURFACE, SEVERAL FASTENERS AT XIFH 159 FOUND LOOSE. R & R WITH NEW FASTENERS IAW SRM 51-35-01, REV 52. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304260862](https://openairdocs.org/sdr/FDEA201304260862.md): Seat Track · corroded · Apr 26, 2013 · N580FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > EXFOLIATION CORROSION FOUND ON SEAT TRACK BASE AT BS 491 TO 502, X= -27.5. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304240840](https://openairdocs.org/sdr/FDEA201304240840.md): Skin · misrepaired · Apr 24, 2013 · N580FE · Doug MD11F · Wing, Plate/Skin
  > RT WING FIXED L/E SURFACE TELESCOPIC DUCT CUT-OUT AREA MISREPAIRED. REPAIRED IAW SRM 57-40-01, REPAIR 10, FIGURE 201, REV 52 AND EA 1-5730-166121. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304240843](https://openairdocs.org/sdr/FDEA201304240843.md): Skin · delaminated · Apr 24, 2013 · N580FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING OTBD FLAP T/E WEDGE INBD EDGE FORM DELAMINATED FROM XOFH 458.690 TO XOFH 468.690. REPAIRED IAW EA 1-5750-166120. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.
- [SDR FDEA201304240842](https://openairdocs.org/sdr/FDEA201304240842.md): Skin · cracked · Apr 24, 2013 · N580FE · Doug MD11F · Trailing Edge Flaps
  > LT WING INBD FLAP UPPER SKIN AT XIFH= 171, 52" FROM T/E FOUND WITH 1 INCH CRACK. REPAIRED IAW EA 1-5750-166124. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304240841](https://openairdocs.org/sdr/FDEA201304240841.md): Skin · cracked · Apr 24, 2013 · N580FE · Doug MD11F · Leading Edge Devices
  > RT WING NR 5 SLAT LOWER SURFACE FOUND CRACK ABOUT 5 INCHES LONG AT XOS 717. REPAIRED IAW EA 1-5750-166127, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304240839](https://openairdocs.org/sdr/FDEA201304240839.md): Access Panel · corroded · Apr 24, 2013 · N580FE · Doug MD11F · Wing, Plate/Skin
  > RT WING T/E LOWER ACCESS PANEL 641JB CUT-OUT FWD EDGE LOWER CAP SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5710-166116. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304230831](https://openairdocs.org/sdr/FDEA201304230831.md): Frame · misrepaired · Apr 23, 2013 · N580FE · Doug MD11F · Fuselage Main, Frame
  > FRAME MISREPAIRED AT CABIN BS 535, L24L. REPAIRED IAW SRM 53-20-07, FIG 201, REPAIR 1, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304230830](https://openairdocs.org/sdr/FDEA201304230830.md): Frame · misrepaired · Apr 23, 2013 · N580FE · Doug MD11F · Fuselage Main, Frame
  > FRAME MISREPAIRED AT CABIN STATION 535, L19L. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 52. EO 1-5100-7-5001B3, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201201260347](https://openairdocs.org/sdr/FDEA201201260347.md): Pressure Switch · failed · Jan 26, 2012 · N580FE · Doug MD11F · Engine Oil Quantity
  > MAX POWER TAKE OFF, NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE INDICATED NORMAL ON GAUGES. ABORT WAS ACCOMPLISHED AT 20 KIAS. LIGHT WENT OUT WHEN POWER MOVED TO IDLE. ALL OIL INDICATIONS REMAINED NORMAL. R & R LOW OIL PRESSURE SWITCH IAW
- [SDR FDEA201108243450](https://openairdocs.org/sdr/FDEA201108243450.md): Hinge · cracked · Aug 24, 2011 · N580FE · Doug MD11F · Fuselage, Door Hinge
  > RIGHT MLG DOOR-CENTER HINGE ASSY FOUND CRACKED. CRACKED HINGE REMOVED AND REPLACED WITH NEW HINGE AT RIGHT HAND DOOR CENTER AREA AS PER SRM 51-35-01 REV 47. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.
- [SDR FDEA201108173313](https://openairdocs.org/sdr/FDEA201108173313.md): Skin · corroded · Aug 17, 2011 · N580FE · Doug MD11F · Fuselage Main, Plate/Skin
  > RT FUSELAGE SKIN BENEATH AFT BODY FAIRING (UPPER SIDE) FROM BS 2155 TO 2164, FOUND CORRODED AT SEVERAL LOCATIONS. CORROSION REMOVED IAW SRM 51-70-01, FIG 201. REPAIR 3 REV 47. ORIGINAL THICKNESS 0.0125", MATERIAL REMOVED 0.085", REMAINING THICKNESS 0.040"
- [SDR FDEA201108173312](https://openairdocs.org/sdr/FDEA201108173312.md): Skin · corroded · Aug 17, 2011 · N580FE · Doug MD11F · Fuselage Main, Plate/Skin
  > RT FUSELAGE BENEATH AFT BODY FAIRING (LOWER SIDE) FROM STA 2155 TO 2164 FOUND CORRODED AT SEVERAL LOCATIONS. CORROSION REMOVED, ORIGINAL THICKNESS 0.095", MATERIAL REMOVED 0.045", REMAINING THICKNESS 0.050". REPAIR CARRIED OUT IAW SRM 53-70-01, FIG 201, REP
- [SDR FDEA201006262195](https://openairdocs.org/sdr/FDEA201006262195.md): Probe · failed · Jun 26, 2010 · N580FE · Doug MD11F · Fuel Indicating System
  > AT LEVEL OFF CALM AIR GOT A FUEL QTY/FUEL USED LEVEL 2 POSSIBLE FUEL LEAK ALERT. FOLLOWED QRH PROCEEDURE S AND ISOLATED PROBLEM TO NR 2 MAIN TANK ERRONEOUS QTY OF - 4500. QTY IN TANK 2 WOLD FLUCTUATE IN MANUAL AND AUTO. NO LEAK NOTED. REMOVED AND REPLACED
- [SDR FDEA201002170442](https://openairdocs.org/sdr/FDEA201002170442.md): Brake · failed · Feb 17, 2010 · N580FE · Doug MD11F · Landing Gear Brake System
  > AFTER TAKEOFF NR 8 BRAKE TEMP CLIMBED TO OVER 400 DEGREES BEFORE DECREASING. AFTER LANDING NR 8 BRAKE RAN HOTTER THAN THE OTHERS. GEAR WAS LOWERED TO COOL BRAKE AND RETRACTED. ACFT LANDED OK WITHOUT INCIDENT. R & R NR 8 BRAKE IAW MM 32-43-20-4. OPS CHECK
- [SDR FDEA200909183325](https://openairdocs.org/sdr/FDEA200909183325.md): Skin · corroded · Sep 18, 2009 · N580FE · Doug MD11F · Wing, Plate/Skin
  > CORROSION - RT UPPER WING SURFACE AT XORS197. REPAIRED IAW EA 1-5710-132215.
- [SDR FDEA200909063264](https://openairdocs.org/sdr/FDEA200909063264.md): Skin · corroded · Sep 6, 2009 · N580FE · Doug MD11 · Wing, Plate/Skin
  > LT WING UPPER SKIN AT STA, XORS 378 FOUND CORROSION. REPAIR IAW EA 1-5710-132212 TITLE: "WINGS-LT WING UPPER SKIN SURFACE CORROSION - REPAIR"
- [SDR FDEA200909063263](https://openairdocs.org/sdr/FDEA200909063263.md): Skin · corroded · Sep 6, 2009 · N580FE · Doug MD11F · Wing, Plate/Skin
  > LT WING UPPER SKIN AT STA, XORS 130 TO XORS 197 FOUND CORROSIONS. REPAIR IAW EA 1-5710-132213 TITLE: "WINGS-LT WING UPPER SKIN SURFACE CORROSION - REPAIR"
- [SDR FDEA200909063262](https://openairdocs.org/sdr/FDEA200909063262.md): Skin · corroded · Sep 6, 2009 · N580FE · Doug MD11F · Wing, Plate/Skin
  > LT WING UPPER SKIN AT STA. XORS 402 TO XORS 433 FOUND CORROSIONS. REPAIR IAW EA 1-5710-132212.
- [SDR FDEA200909013226](https://openairdocs.org/sdr/FDEA200909013226.md): Skin · corroded · Sep 1, 2009 · N580FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT UPPER WING SKIN HAS CORROSION AT STA XORS 150. REPAIRED IAW EA 1-5750-132215.
- [SDR FDEA200909013225](https://openairdocs.org/sdr/FDEA200909013225.md): Skin · corroded · Sep 1, 2009 · N580FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT UPPER WING SKIN HAS CORROSION, STA XORS 163. REPAIRED IAW EA 1-5710-132215.
- [SDR FDEA200909013224](https://openairdocs.org/sdr/FDEA200909013224.md): Skin · corroded · Sep 1, 2009 · N580FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT UPPER WING SKIN HAS CORROSION, STA XORS 298. REPAIRED IAW EA 1-5710-132215. MAJOR REPAIR.
- [SDR FDEA200909013223](https://openairdocs.org/sdr/FDEA200909013223.md): Skin · corroded · Sep 1, 2009 · N580FE · Doug MD11F · Wing, Plate/Skin
  > LEFT UPPER WING SKIN STA XORS 317 TO 360 HAS CORROSION. REPAIR IAW EA 1-5750-132209.
- [SDR FDEA200909013222](https://openairdocs.org/sdr/FDEA200909013222.md): Longeron · corroded · Sep 1, 2009 · N580FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LONGERON 45R BS879 LWR OTBD SURFACE CORRODED IN FWD CARGO. COMPLIED WITH EA 1-5310-132210: FUSELAGE - LONGERON 45R CRACK AT APPROX STA 879 - REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 107.
- [SDR FDEA200909013201](https://openairdocs.org/sdr/FDEA200909013201.md): Longeron · corroded · Sep 1, 2009 · N580FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > FWD CARGO - LONGERON 45R AT BS 879 LWR OTBD SURFACE CORRODED. COMPLIED WITH EA 1-5310-132210: FUSELAGE - LONGERON 45R CRACK AT APPROX STA 879 - REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV. 107
- [SDR FDEA200908313193](https://openairdocs.org/sdr/FDEA200908313193.md): Skin Panel · cracked · Aug 31, 2009 · N580FE · Doug MD11F · Wing, Plate/Skin
  > 25EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN INSP AT RT LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. REPAIR IAW EA 1-5710-133858 TITLE: "AD2007-07-04 - WINGS - RT LWR SKIN PLANK CUTOUT AT 636AB - REPAIR TO ACCESS DOOR A
- [SDR FDEA200908313192](https://openairdocs.org/sdr/FDEA200908313192.md): Skin Panel · cracked · Aug 31, 2009 · N580FE · Doug MD11F · Wing, Plate/Skin
  > 21 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT W LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. REPAIR IAW EA 1-5710-133857 TITLE: "AD2007-07-04 - WINGS - LT LWR SKIN PLANK CUTOUT AT 536AB - REPAIR TO A

Next page: https://openairdocs.org/deregistered/N580FE-2024-03-02/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N580FE' AND deregistration_id = 'N580FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N580FE-2024-03-02/reports

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